Gas turbine engine internal insulation

ABSTRACT

The invention is concerned with an improvement in a modular gas turbine engine assembly comprising a tubular case, a gasifier module detachably attachable with a first end thereof adjacent a first end of said case and a power output module detachably attachable with a first end thereof adjacent a second end of said case, said case and said modules defining a partially walled off combustion-ducting section within said engine. The improvement comprises a plurality of individually replaceable insulation packs which provide heat insulation between the combustion-ducting section walls and each of said case, said gasifier module and said power output module. In another sense the invention comprises an improved individually replaceable insulating pack comprising a high temperature resistant metallic sheet having a porous insulation blanket and including a fine mesh of wire covering the surface of the blanket which is not adjacent to the sheet and holding the blanket against the sheet.

BACKGROUND OF THE INVENTION

1. Field of the Invention

The invention is concerned with insulation and more particularly with animproved insulation pack. Even more particularly the invention isconcerned with the use of a plurality of individually replaceableinsulation packs for providing heat insulation between a combustionsection of a modular gas turbine engine assembly and the case, thegasifier module and the power output module of such an assembly.

2. Prior Art

The prior art, for example U.S. Pat. Nos. 3,310,904; 3,304,054;3,321,179; and 3,775,979, discloses the use of insulation within gasturbine engines. While insulation per se for use within a gas turbineengine is well known, the prior art has failed to teach the use of aplurality of individually replaceable insulation packs to provide heatinsulation between a combustion-ducting section of such an engine andeach of the case, the gasifier module and the power output modulethereof. Thus, it has been generally customary to make the case of suchan engine out of a high temperature resistant material such as a highnickel content alloyed steel. Also, the prior art has failed to teachthe provision of such packs which are easily individually removable forreplacement. The present invention provides an improvement which isparticularly useful in a modular gas turbine engine assembly and whereina plurality of individually replaceable insulation packs are providedwhich allow the use of plain carbon steel rather than a high temperaturenickel based alloyed steel for the case of the engine.

SUMMARY OF THE INVENTION

In one sense, the invention comprises an improvement in a modular gasturbine engine assembly comprising a tubular case, a gasifier moduledetachably attachable with a first end thereof adjacent a first end ofsaid case and a power output module detachably attachable with a firstend thereof adjacent a second end of said case, said case and saidmodule defining a partially walled off combustion-ducting section withinsaid engine. The improvement comprises a plurality of individuallyreplaceable insulation packs providing heat insulation between saidcombustion-ducting section and each of said case, said gasifier moduleand said output module.

In another sense, the invention comprises an individually replaceableinsulation pack comprising a high temperature resistant metallic sheethaving a porous insulation blanket held against the sheet by a fine meshof metal which covers the surface of the blanket which is not adjacentto the sheet. Generally, the metallic sheet is bendable so that suchinsulation packs are sufficiently deformable to be individuallyreplaceable within a gas turbine engine assembly.

BRIEF DESCRIPTION OF THE DRAWINGS

The invention will be better understood by reference to the Figures ofthe drawings wherein like numbers denote like parts throughout andwherein:

FIG. 1 illustrates in side section a modular gas turbine engine assemblywhich includes the improvement of the present invention;

FIG. 2 illustrates in perspective an insulation pack in accordance withthe present invention and as used in the engine assembly illustrated inFIG. 1; and

FIG. 3 illustrates, in section, another insulation pack in accordancewith the present invention.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT

Referring first to FIG. 1 there is illustrated therein a modular gasturbine engine 10 which includes the improvement of the presentinvention. Such an engine is described in considerably more detail inU.S. patent application Ser. No. 630,476 filed Nov. 10, 1975 andcommonly assigned hereiwith. The disclosure of said application Ser. No.630,476 with respect to the structure and operation of such an engine ishereby referred to and incorporated herein by reference thereto.Briefly, the engine 10 includes a tubular case 12 a gasifier module 14and a power output module 16. A first end 18 of the gasifier module 14is detachably attached to a first end 20 of the tubular case 12. A firstend 22 of the power output module 16 is detachably attached to a secondend 24 of the tubular case 12. The case 12, the gasifier module 14 andthe power output module 16 together define a partially walled offcombustion-ducting section 26 with the walls thereof comprising a firstinwardly extending flange 28, an exterior wall 30 of the case 12, and asecond inwardly extending flange 32 with the first inwardly extendingflange 28 extending from the gasifier module 14 and the second inwardlyextending flange 32 extending from the power output module 16.

The present invention is particularly concerned with an improvementwhich comprises a plurality of individually replaceable insulation packs34 which fit together to provide heat insulation between thecombustion-ducting section 26 and each of the tubular case 12, thegasifier module 14 and the power output module 16. It is of courseunderstood that the partially walled off combustion-ducting section 26is not completely walled off from either the gasifier module 14 or thepower output module 16 since a gasifier module shaft 36 and a gasifierturbine 38 must pass from the gasifier module 14 into the walledcombustion-ducting section 26 and in like manner a power output shaft 40and a power turbine 42 must pass from the power output module 16 intothe walled combustion-ducting section 26 and, of course, provision mustbe made for gas flow into and out of the combustion-ducting section 26.

As will be noted by reference to FIG. 1 first bolt means 44 serve tofasten the tubular case 12 to the gasifier module 14 while second boltmeans 46 serve to fasten the power output module 16 to the tubular case12. Thus, and as is explained in considerably more detail in thepreviously mentioned application Ser. No. 630,476, it is clear that thegasifier module 14 can be removed from the tubular case 12 and likewisethe power output module 16 can be removed therefrom simply by removingrespective of the bolt means 44 and/or 46.

With the tubular case 12, the gasifier module 14 and the power outputmodule 16 separated from one another, each of the insulation packs 34can be easily removed and replaced as required. The pack 34a for examplecan be in the form of a sleeve which is slit longitudinally at a slit47. To remove the pack 34a all that is necessary is to grasp the sleeveadjacent the longitudinal slitting thereof and to pull it out fromaround the first inwardly extending flange 28. Generally the pack 34awill be formulated so as to springably grasp the flange 28 when it is inposition thereabout. The insulation pack 34c can be in the form of acomplete ring and can be simply removed by lifting it out rightwardlyfrom the gasifier module 14 once it has been separated from the tubularcase 12. The insulation pack 34b, after removal of the insulation packs34a and 34c, can be removed by simply lifting it rightwardly away fromthe gasifier module 14. The insulation pack 34d can be removed similarlyto the insulation pack 34c or similarly to the insulation pack 34a if itis slit as is the insulation pack 34a. The insulation pack 34e and theinsulation pack 34f can also be removed similarly to the insulation pack34c. The insulation packs 34g and 34h can be removed from the tubularcase 12 once the power output module 16 has been removed therefrom. Theinsulation pack 34i would generally be similarly slit and removed in asimilar manner to the insulation pack 34a. The insulation packs 34j and34k are generally removed similarly to the insulation pack 34c. Theinsulation pack 34l would generally be removed similarly to theinsulation pack 34a. Insulation pack 34m would be removed leftwardlyfrom the power output module 16 after it had been disconnected from thetubular case 12. Insulation pack 34m like insulation pack 34a wouldpreferably include a slit therein to allow it to be more easily removed.

Turning now most particularly to FIGS. 2 and 3 there is illustratedtherein most thoroughly the structure of the insulation packs 34.Briefly, each of the insulation packs 34 comprises a high temperatureresistant metallic sheet 48 having held against a first side 49 thereofa porous insulation blanket 50. It is useful that the insulation blanket50 be porous since this assures that the insulation blankets are in noway used as a pressure vessel and that hence the high temperatureresistant metallic sheet 48 can be made relatively flexible and thin anddoes not have to provide sufficient strength to hold pressure. Further,in such structures as pack 34a it is desirable to formulate sheet 48 ofspring metal whereby the blanket 50 will be biased thereby to grasp theflange 28. The porous insulation blanket 50 is abutted as illustrated inFIG. 1 against a wall portion, e.g., the first inwardly extending flange28, the exterior wall 30 of the tubular case 12, the second inwardlyextending flange 32 or an inwardly extending structural member 52 all ofwhich together comprise the wall portions of the partially walled offcombustion section 26 and the metallic sheet 48 is thereby spaced fromthe appropriate wall portion of the partially walled offcombustion-ducting section 26 by the thickness of the porous insulationblanket 50. Each of the insulation packs 34 generally includes a finemesh or screen 54 of metal which covers a surface 56 of the insulationblanket 50 which is not abutting the sheet 48. Each of the screens 54 isattached to the respective sheet 48 at the joinder 57 as by welding,riveting, screwing or the like. The insulation blanket 50 preferablycomprises interlaced ceramic fibers 58 and a binder is generally notused in the blanket to bind the fibers to one another so that theblanket 50 will remain sufficiently porous. Also, no bonding agent isgenerally used to bond the blanket 50 to the sheet 48 thus eliminatingany problem of bonding agent deterioration and providing addedflexibility. It is preferred that the fibers comprise an aluminosilicatefire clay. When insulation packs 34 are utilized as in the improvementof the present invention it has been found that the tubular case 12along with the first flange 28 and the second flange 32 can beformulated of relatively inexpensive carbon steel rather than of a moreexpensive high nickel content steel alloy.

It will be noted that each of the insulation packs 34 is generally sizedto be held in position against adjacent of the insulation packs 34.Thus, each pack can be made of a size and shape which makes it easilyremovable and replaceable. Further, it is not necessary to remove orreplace the entire insulation within an engine 10 when a portion of theinsulation material may have become damaged in one manner or another.Still further, the individual insulation packs 34 are easily removablewhen necessary for servicing of other internal engine components orparts. With all of the insulation within the engine, the engine can besteam cleaned whenever necessary. Further still, the insulation packs 34will hold unburned fuel because of their porous nature until it eitherdrains out of fuel drains which can be provided for this purpose orvaporizes or burns out of the insulation packs 34.

While the invention has been described in connection with specificembodiments thereof, it will be understood that it is capable of furthermodification, and this application is intended to cover any variations,uses or adaptations of the invention following, in general, theprinciples of the invention and including such departures from thepresent disclosure as come within known or customary practice in the artto which the invention pertains and as may be applied to the essentialfeatures hereinbefore set forth, and as fall within the scope of theinvention and the limits of the appended claims.

We claim:
 1. In a modular gas turbine engine assembly comprising atubular case, a gasifier module detachably attachable with a first endthereof adjacent a first end of said case and a power output moduledetachably attachable at a first end thereof adjacent a second end ofsaid case, said case and said modules defining a partially walled offcombustion-ducting section within said engine, an improvement comprisinga plurality of individually replaceable insulation packs providing heatinsulation between said combustion-ducting section and each of saidcase, said gasifier module and said power output module, each of saidpacks comprising a high temperature resistant metallic sheet having heldagainst a first side thereof a porous insulation blanket with a finemesh of metal attached to said sheet and covering the surface of saidblanket not abutted to said sheet and wherein said blanket is abuttedagainst a wall portion of said combustion-ducting section with saidsheet being spaced therefrom by the thickness of said blanket, saidblanket not being bonded to said sheet by a bonding agent and a bindernot being used in said blanket to bind said fibers to one another.
 2. Animprovement as in claim 1, wherein each of said blankets compriseinterlaced ceramic fibers.
 3. An improvement as in claim 2, wherein saidfibers comprise an aluminosilicate fire clay.
 4. An improvement as inclaim 3, wherein said case comprises carbon steel.
 5. An improvement asin claim 1, wherein said sheet comprises spring metal.